Equipment Overview
Explore the functions and specifications of the equipment operated by our center at a glance.
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Altitude Environmental Chamber
This chamber precisely reproduces various high-altitude flight conditions—including low pressure and low temperature—on the ground. It is used to evaluate the reliability of electrical components and key systems by verifying their ability to operate prope
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Equipment Details
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Key Feature
- Test Category: Performance Testing under Aircraft Operating Environments
- Test criteria are assigned based on the operating conditions expected for AAV flight.
- Environmental simulation tests—such as altitude, temperature, and humidity—are required for AAV component evaluation.
- Performance measurements for mechanical and avionics components are conducted under specified environmental conditions.
- A test chamber designed for evaluating the performance and durability of AAV/UAM onboard components and modules.
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Inside View of the Altitude Environmental Chamber
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Test Data Graph
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Specification
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Size External: W 3,778 × D 6,513 × H 5,517 mm Internal: W 3,000 × D 5,000 × H 2,100 mm Temperature Range -70°C to +100°C Humidity Range 20% to 98% RH Temperature Change Rate (Linear) Heat Up: 20°C to +80°C within 30 minutes (No Load) ,Cool Down: 20°C to -56°C within 38 minutes (No Load) Test Altitude Up to 1 km Temperature & Humidity Accuracy ±1°C / ±2% RH Altitude Uniformity ±0.5% Altitude Change Rate 100m/min Cooling Method Air-cooled Control System PC-based central control
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